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The Saturn I (pronounced "Saturn one") was a rocket designed as the United States' first medium-lift launch vehicle for low Earth orbit payloads. The rocket's first stage was built as a cluster of propellant tanks engineered from older rocket tank designs. Its development was taken over from the Advanced Research Projects Agency in 1958 by the newly-formed civilian NASA. Its design proved sound and flexible. It was successful in initiating the development of liquid hydrogen-fueled rocket propulsion, launching the Pegasus satellites, and flight verification of the Apollo command and service module launch phase aerodynamics.
Missions
10
Success Rate
100.0%
Successes
10
Failures
0
Success Streak
10
Partial Failures
0
Active 1964 to 1965
Rocket
Height: 55m
Payload to Orbit
LEO: 9,070 kg
Liftoff Thrust
6,700 Kilonewtons
Stages
2
Active 1961 to 1963
Rocket
Height: 55m
Liftoff Thrust
6,700 Kilonewtons
Stages
1